메뉴 건너뛰기




Volumn 16, Issue 6, 2000, Pages 1125-1131

Performance analysis for high-speed missile inlets

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DIFFUSERS (FLUID); MATHEMATICAL MODELS; MISSILES; NAVIER STOKES EQUATIONS; SUBSONIC AERODYNAMICS;

EID: 0034324645     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5687     Document Type: Article
Times cited : (6)

References (16)
  • 1
    • 21744456652 scopus 로고    scopus 로고
    • Automated optimal design using CFD and high performance computing
    • edited by J. Palma and J. Dongarra Springer-Verlag Berlin
    • Knight D. D. Automated Optimal Design Using CFD and High Performance Computing edited by J. Palma and J. Dongarra Lecture Notes in Computer Science Vol. 1215 Springer-Verlag Berlin 1997 pp. 198-221.
    • (1997) Lecture Notes in Computer Science , vol.1215 , pp. 198-221
    • Knight, D.D.1
  • 2
    • 0031095642 scopus 로고    scopus 로고
    • Automated design optimization for the P2 and P8 hypersonic inlets
    • Shukla V. Gelsey A. Schwabacher M. Smith D. and Knight D. "Automated Design Optimization for the P2 and P8 Hypersonic Inlets, " Journal of Aircraft Vol. 34 No. 2 1997 pp. 228-235.
    • (1997) Journal of Aircraft , vol.34 , Issue.2 , pp. 228-235
    • Shukla, V.1    Gelsey, A.2    Schwabacher, M.3    Smith, D.4    Knight, D.5
  • 3
    • 0032208514 scopus 로고    scopus 로고
    • Automated optimal design of two-dimensional supersonic missiles inlets
    • Blaize M. Knight D. and Rasheed K. "Automated Optimal Design of Two-Dimensional Supersonic Missiles Inlets, " Journal of Propulsion and Power Vol. 14 No. 6 1998 pp. 850-898.
    • (1998) Journal of Propulsion and Power , vol.14 , Issue.6 , pp. 850-898
    • Blaize, M.1    Knight, D.2    Rasheed, K.3
  • 5
    • 84983210776 scopus 로고    scopus 로고
    • Automated optimization of two-dimensional high speed missile inlets
    • Jan
    • Blaize M. and Knight D. "Automated Optimization of Two-Dimensional High Speed Missile Inlets, " AIAA Paper 98-0950 Jan. 1998.
    • (1998) AIAA Paper 98-0950
    • Blaize, M.1    Knight, D.2
  • 7
    • 0342671043 scopus 로고    scopus 로고
    • Navier-stokes simulation methodology for supersonic missiles inlets
    • Sept
    • Montazel X. Kergaravat Y. and Blaize M. "Navier-Stokes Simulation Methodology for Supersonic Missiles Inlets, " AIAA Paper 97-3147 Sept. 1997.
    • (1997) AIAA Paper 97-3147
    • Montazel, X.1    Kergaravat, Y.2    Blaize, M.3
  • 8
    • 0343541320 scopus 로고    scopus 로고
    • Der druckruckgewinn bei geschossen mit ruckstossantrieb bei hohen uberschallgeschwindeigkeiten (der wirkungsgrad von stossdiffusoren)
    • Bericht
    • Oswatitsch K. "Der Druckruckgewinn bei Geschossen mit Ruckstossantrieb bei hohen Uberschallgeschwindeigkeiten (der Wirkungsgrad von Stossdiffusoren), " Forschungen und Entwicklungen des Heereswaffenamtes Bericht Nr. 1005.
    • Forschungen und Entwicklungen des Heereswaffenamtes , Issue.1005
    • Oswatitsch, K.1
  • 11
    • 0004237080 scopus 로고    scopus 로고
    • Numerical simulation of HSCT inlet operability with angle of attack
    • July
    • Zha G. C. Knight D. D. Smith D. and Haas M. "Numerical Simulation of HSCT Inlet Operability with Angle of Attack, " AIAA Paper 97-2761 July 1997.
    • (1997) AIAA Paper 97-2761
    • Zha, G.C.1    Knight, D.D.2    Smith, D.3    Haas, M.4
  • 12
    • 0343541318 scopus 로고    scopus 로고
    • Diffuser design and performance analysis by unified integral methods
    • July
    • Johnston J. P. "Diffuser Design and Performance Analysis by Unified Integral Methods." AIAA Paper 97-2733 July 1997.
    • (1997) AIAA Paper 97-2733
    • Johnston, J.P.1
  • 13
    • 0020587486 scopus 로고
    • A computational method for subsonic compressible flow in diffusers
    • Jan
    • Childs R. E. and Ferziger J. H. "A Computational Method for Subsonic Compressible Flow in Diffusers, " AIAA Paper 83-0505 Jan. 1983.
    • (1983) AIAA Paper 83-0505
    • Childs, R.E.1    Ferziger, J.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.